FIELD: military equipment, in particular, warheads, applicable in development of various ammunitions, including warheads with a parachute stabilization system for salvo-fire jet projectiles. SUBSTANCE: warhead has a body, warhead section, section with the parachute stabilization system, actuator, powder charge, bottom, cover, movable base, pusher, booster components, stop, expansion chamber and gas passages. The section with the parachute stabilization system is furnished with a diaphragm made in the form of a cup with peripherally located gas passages and attached to the body. A high-pressure chamber is formed between the diaphragm and bottom, the pusher is installed in the longitudinal axis, and on one side it is fixed to the movable base, and on the other side it is connected through a flexible coupling to the parachute stabilization system packed around the pusher. The actuator is positioned inside the diaphragm, and the powder charge - in the high-pressure chamber, which has a gas-dynamic coupling with the expansion chamber through gas passages. EFFECT: enhanced reliability of functioning at angular velocities typical for spinning projectiles, improved structural characteristics. 2 dwg
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Authors
Dates
2000-01-20—Published
1999-06-16—Filed